Fatigue Fracture of a Fuel Line at a Butt Weld

{"title":"Fatigue Fracture of a Fuel Line at a Butt Weld","authors":"","doi":"10.31399/asm.fach.aero.c0047590","DOIUrl":null,"url":null,"abstract":"\n A weld in a fuel-line tube broke after 159 h of engine testing. The 6.4-mm (0.25-in.) OD x 0.7-mm (0.028-in.) wall thickness tube and the end adapters were all of type 347 stainless steel. The butt joints between tube and end adapters were made by automated gas tungsten arc (orbital arc) welding. It was found that the tube had failed in the HAZ. Examination of a plastic replica of the fracture surface in a transmission electron microscope established that the crack origin was at the outer surface of the tube. The crack growth was by fatigue; closely spaced fatigue striations were found near the origin, and more widely spaced striations near the inner surface. The quality of the weld and the chemical composition of the tube both conformed to the specifications. However, the fuel-line assembly had vibrated excessively in service. The fuel-line fracture was caused by fatigue induced by severe vibration in service. Additional tube clamps were provided to damp the critical vibrational stresses. No further fuel-line fractures were encountered.","PeriodicalId":326464,"journal":{"name":"ASM Failure Analysis Case Histories: Air and Spacecraft","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"ASM Failure Analysis Case Histories: Air and Spacecraft","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.31399/asm.fach.aero.c0047590","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
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Abstract

A weld in a fuel-line tube broke after 159 h of engine testing. The 6.4-mm (0.25-in.) OD x 0.7-mm (0.028-in.) wall thickness tube and the end adapters were all of type 347 stainless steel. The butt joints between tube and end adapters were made by automated gas tungsten arc (orbital arc) welding. It was found that the tube had failed in the HAZ. Examination of a plastic replica of the fracture surface in a transmission electron microscope established that the crack origin was at the outer surface of the tube. The crack growth was by fatigue; closely spaced fatigue striations were found near the origin, and more widely spaced striations near the inner surface. The quality of the weld and the chemical composition of the tube both conformed to the specifications. However, the fuel-line assembly had vibrated excessively in service. The fuel-line fracture was caused by fatigue induced by severe vibration in service. Additional tube clamps were provided to damp the critical vibrational stresses. No further fuel-line fractures were encountered.
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对接焊缝燃油管路的疲劳断裂
发动机测试159小时后,燃油管的焊缝破裂。6.4毫米(0.25英寸)外径x 0.7毫米(0.028英寸)壁厚管和端适配器都是347型不锈钢。管与端接头对接采用自动气体钨弧焊(轨道弧焊)。发现管子在防空区失效了。在透射电子显微镜下对断裂表面的塑料复制品进行检查,确定裂纹起源于管的外表面。裂纹扩展以疲劳扩展为主;在原点附近发现了密集分布的疲劳条纹,而在内表面附近发现了更宽分布的疲劳条纹。焊接质量和管的化学成分都符合规范。然而,燃油管路组件在使用过程中振动过大。燃油管路断裂是由使用过程中剧烈振动引起的疲劳引起的。额外的管夹被用来抑制临界振动应力。没有发现进一步的燃料管道断裂。
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